794814: CASE,COMPRESSOR,AIRCRAFT GAS TUR.
CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 50.500 INCHES NOMINAL IN, material: STEEL COMP 410 OVERALL, design_type: COMPRESSOR, overall_length: 4.000 INCHES NOMINAL IN, special_features: T.O. 2J-TF33-4; GOES ON THE 1ST STAGE COMPRESSOR OUTER, end_item_identification: TF33 AIRCRAFT ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-305-5309, indicating validated use in U.S. government and defense logistics supply chains.
Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| diameter | 50.500 INCHES NOMINAL IN |
| material | STEEL COMP 410 OVERALL |
| design_type | COMPRESSOR |
| overall_length | 4.000 INCHES NOMINAL IN |
| special_features | T.O. 2J-TF33-4; GOES ON THE 1ST STAGE COMPRESSOR OUTER |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-305-5309 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 50.500 INCHES NOMINAL IN |
| OVERALL LENGTH | 4.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-TF33-4; GOES ON THE 1ST STAGE COMPRESSOR OUTER |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| MATERIAL | STEEL COMP 410 OVERALL |
No substitute or cross-reference records for this part.